Douglas DC-8-73F

Service difficulty reports · 15,471

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC873F'
  ORDER BY difficulty_date DESC"

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SDR UPS07850407Angle · crackedINSPECTION TYPE:C2 LT HORIZ STAB UPPER MOVEABLE FAIRING MOST AFT H-ANGLE CRACKED. REMOVED AND REPLACED LT HORIZ STAB MOVEABLE FAIRING AFT H-ANGLE IAW SRM 51-03-00-0, DWG 3702464, AND SRM 51-03-02.Jul 21, 2007 · N851UP · Doug DC873F · Horizontal Stabilizer Miscellaneous StructureSDR UPS07850396Angle · crackedINSPECTION TYPE:C2 RT HORIZ STAB MOVEABLE FAIRING 2ND AFT H-ANGLE UPPER, CRACKED. REMOVED CRACKED H-ANGLE ON RT HORIZ STAB MOVEABLE FAIRING IAW SRM 51-03-00-0. FABRICATED AND INSTALLED RT HORIZ STAB FAIRING ATTACH H-ANGLE IAW SRM 51-03-02, DWG 3702464, AND SJul 21, 2007 · N851UP · Doug DC873F · Horizontal Stabilizer Miscellaneous StructureSDR UPS07850393Angle · crackedINSPECTION TYPE:C2 RIGHT HORIZ STAB FRONT SPAR INBOARD LWR ANGLE CRACKED. REMOVED AND REPLACED RIGHT HORIZ STAB FRONT SPAR INBOARD LWR ANGLE IAW SRM 51-3-0, 51-1-20D, SRM 51-3-2, AND DC8 AMM 55-10-00-2.Jul 21, 2007 · N851UP · Doug DC873F · Horizontal Stabilizer Miscellaneous StructureSDR UPS07850388Frame · crackedINSPECTION TYPE:C2 STA 70 FRAME CRACKED AND CORRODED BETWEEN L31R AND L32R IN A/C COMPT. REPAIRED CRACKED AND CORRODED FRAME AT STA 70 BETWEEN L31R AND L32R IN A/C BAY IAW SRM 53-02-05 FIG 08C2.Jul 20, 2007 · N851UP · Doug DC873F · Fuselage Main, FrameSDR UPS07850397Skin · crackedINSPECTION TYPE:C2 FUSE SKIN CRACKED AND BULGING AT STA 1692 L28R. REPAIRED FUSELAGE EXTERIOR SKIN AT STA 1692 L28R IAW UPS EO DC8- 5330-20248-D APPX E AND SRM SRO8530032.Jul 18, 2007 · N851UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07850395Skin · damagedINSPECTION TYPE:C2 CREASE ON UPPER FUSE SKIN AT STA 1800 L9L. CUT OUT DAMAGED AREA ON FUSE SKIN AT STA 1800 L9L IAW SRM 53-2-1 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, AND FILLER AT STA 1800 L9L IAW SRM 53-2-1 FIG 7, AND SRM 53-5-3 FIG 1 SHEET 1.Jul 18, 2007 · N851UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07850345Doubler · puncturedINSPECTION TYPE:C2 LEFT WING INBOARD FLAP STA 110 UPPER SURFACE SKIN DENT AND EXISTING DOUBLER PUNCTURED. REMOVED DAMAGED DOUBLER ON LEFT WING INBOARD FLAP STA 110 UPPER SURFACE IAW SRM 51-01-21-0. FABRICATED AND INSTALLED REPAIR DOUBLER AT LEFT WING UPPER SJul 18, 2007 · N851UP · Doug DC873F · Trailing Edge FlapsSDR UPS07850339Skin · gougedINSPECTION TYPE:C2 LH INBD UPPER SURFACE SKIN EXSISTING REPAIR DOUBLER HAS DEEP GOUGE AT STA 100 REMOVED DAMAGED DOUBLER AT L/WING STA 100 IAW SRM 51-01-21-0 FABRICATED AND INSTALLED REPAIR DOUBLER AT LH WING INBD UPPER SURFACE STA 100 IAW SRM 57-07-01-0 AJul 18, 2007 · N851UP · Doug DC873F · Wing, Plate/SkinSDR UPS07850194Floor Panel · damagedINSPECTION TYPE:N/A HOLE IN CARGO COMPT 33 FLOOR, APPROX LOCATION FS 1069, LBL 40. PERFORMED INTERIM REPAIR IAW EO DC8-5320-8724. ENTERED IN DEFERRED ITEM LOG CONTROL NR D354723. PERFORMED PERMANENT REPAIR PER EO DC8-5320-8724-APP C. THIS CLEARS D354723. Jul 18, 2007 · N867UP · Doug DC873F · Fuselage Floor PanelSDR DHL2007804500Rib · crackedNR 1 STUB WING RIB JOINT ANGLE CRACKED 0.750", STA XFS 529.000. REMOVED CRACKED ANGLE IAW SRM 51-1-21. FABRICATED NEW ANGLE (AL7075"0" 0.080") IAW DWG NR 9753297. HEAT TREATED FROM AL7075"0" TO 7075T6 IAW SRM 51-1-1 PG 1-13-17. CLEANED, TREATED AND PRIMED Jul 16, 2007 · N804DH · Doug DC873F · Wing, Rib/BulkheadSDR UPS07850181Connector · looseINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. SEATED CONNECTOR ON BATTERY PACK & LIGHTS TESTED NORMAL PER 33-50-01 -2.Jul 16, 2007 · N810UP · Doug DC873F · Light System WiringSDR DHL2007804529Skin · misrepairedRT OUTBD FLAP T/E UPPER PANEL HAS A NON-STANDARD REPAIR AT STA XF 375.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW BOEING MSG NR 1-405802434-2 DATED 06-07-07. REMOVED PANEL PLATING WITH EXISTING NON-STANDARD REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICJul 15, 2007 · N804DH · Doug DC873F · Trailing Edge FlapsSDR DHL2007804515Floorbeam · corrodedMAIN CARGO COMPT FLOOR PANEL SUPPORT ANGLE CORRODED, STA 25.000 RBL 26 TO 42. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. CUT OUT CORRODED ANGLE SEGMENT IAW SRM 53-2-0 PG 1. FABRICATED REINFORCING ANGLE (AL7075T6 0.Jul 14, 2007 · N804DH · Doug DC873F · Fuselage Main, Floor BeamSDR DHL2007804502Frame · crackedRT OUTER WING INBD L/E UPPER FORMER CRACKED 0.500" STA XFS 691.250. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-1-8BJul 14, 2007 · N804DH · Doug DC873F · Wing SparSDR DHL2007804501Frame · crackedRT OUTERWING INBD L/E CRACKED 0.500" AT LWR FORMER STA XFS 635.000. REMOVED FASTENERS IAW SRM 51-1-21. PERFORMED STOP HOLE AND FABRICATED (2EA) ANGLE DOUBLER (AL7075T6 0.032") IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLERS IAW SJul 14, 2007 · N804DH · Doug DC873F · Wing SparSDR UPS07850380Skin · gougedINSPECTION TYPE:C2 FUSELAGE EXTERIOR SKIN HAS DEEP GOUGE AND DENT AT STA 160 L21L TO L22L. REPAIR EXTERIOR SKIN IAW SAA EA 008-5330-01-A0966, UPS RAA DC8-53-2064 3.Jul 14, 2007 · N807UP · Doug DC873F · Fuselage Main, Plate/SkinSDR UPS07850225Door Frame · crackedINSPECTION TYPE:C2 L-1 DOOR FRAME SEGMENT CRACKED IN BAYONETTE AREA. STOP DRILLED CRACK IN FRAME SEGMENT AT L-1 DOOR IAW SRM 52-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER ON L-1 DOOR FRAME SEGMENT IAW SRM 52-02-02 FIG 007.Jul 14, 2007 · N807UP · Doug DC873F · Passenger/Crew DoorsSDR UPS07850182Battery Pack · inoperativeINSPECTION TYPE:N/A EMERGENCY LIGHTS ARE VERY DIM. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK OK.Jul 13, 2007 · N809UP · Doug DC873F · Emergency LightingSDR UPS07850180Battery Pack · inoperativeINSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK ASSEMBLY IAW MM 33-50-02-2. OPS CHECK GOOD.Jul 13, 2007 · N868UP · Doug DC873F · Emergency LightingSDR DHL2007804514Floor Panel · corrodedMAIN CARGO COMPT FLOOR PANEL NR 8 UPPER SKIN CORRODED (STA 8.000 - 70.000). REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. REMOVED CORRODED FLOOR PANEL SKIN IAW SRM 51-1-21. FABRICATED NEW FLOOR PANEL SKIN (AL7075T6 0.Jul 12, 2007 · N804DH · Doug DC873F · Fuselage Floor PanelSDR UPS07850227Fitting · crackedINSPECTION TYPE:C2 STA 1180 L27L BANANA FITTING IS CRACKED. REMOVED AND REPLACED BANANA FITTING AT STA 1180 L27L IAW SRM 51-01-20D, AND SRM 51-3-2.Jul 11, 2007 · N807UP · Doug DC873F · Fuselage Main, Attach FittingsSDR UPS07850163Slide · out of positionINSPECTION TYPE:N/A RESTOW ESCAPE SLIDE. RESTOWED ESCAPE SLIDE IAW MM 25-60-01-2.Jul 11, 2007 · N805UP · Doug DC873F · Escape SlideSDR UPS07850216Longeron · crackedINSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L34R. REMOVED END FITTING AT STA 1140 L34R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT END FITTING AT STA 1140 L34R IAW SRM 51-1-20D, AND DWG 475814.Jul 10, 2007 · N807UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850191Fitting · crackedINSPECTION TYPE:C2 LONGERON END FITTING CRACKED AT STA 1140 L35L. REMOVED L35L END FITTING AT STA 1140 IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED L35L END FITTING AT STA 1140 IAW SRM 51-3-2, AND SRM 51-1-20D.Jul 10, 2007 · N807UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850185Fitting · crackedINSPECTION TYPE:C2 LONGERON ATTACH FITTING CRACKED AT STA 1140 L33R. REMOVED LONGERON END FITTING AT STA 1140 L33R IAW SRM 51-1-20D. LOCATED, DRILLED UP, AND INSTALLED LONGERON END FITTING AT STA 1140 L33R IAW SRM 51-3-2, AND SRM 51-1-20D.Jul 10, 2007 · N807UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR UPS07850192Skin · corrodedINSPECTION TYPE:C2 LEFT SIDE OF RUDDER SKIN ZR 251 HAS CORROSION. REMOVED SKIN PANEL ON LEFT SIDE OF RUDDER STA ZR 251 IAW SRM 51-1-21. FABRICATED AND INSTALLED LEFT RUDDER SKIN PANEL AT STA ZR 251 IAW SRM 51-3-2, SRM 51-1-9A, AND DWG 5655077.Jul 8, 2007 · N807UP · Doug DC873F · Rudder, Plate/SkinSDR UPS07850178Skin · canningINSPECTION TYPE:C2 RIGHT SIDE OF RUDDER SKIN ZR 271 HAS OIL CANNING. REMOVED SKIN PANEL ON RT/SIDE OF RUDDER AT ZR 271 IAW SRM 51-1-21. FABRICATED AND INSTALLED RUDDER SKIN PANEL ON RT/SIDE OF RUDDER STA ZR 271 IAW SRM 51-1-21, AND DWG 56555077.Jul 8, 2007 · N807UP · Doug DC873F · Rudder, Plate/SkinSDR UPS07850184Floorbeam · corrodedINSPECTION TYPE:C2 HEAVY CORROSION ON TOP OF FLOORBEAM IN C-PIT TUNNEL AT STA 1300 LBL 51. REMOVED CORROSION FROM FLOORBEAM, FOUND TO BE OUT OF LIMITS IAW SRM 53-2-00. FABRICATED AND INSTALLED REPAIR ANGLES AT STA 1300 LBL 51 FLOORBEAM IAW SRM 53-2-0 FIG 1B.Jul 7, 2007 · N807UP · Doug DC873F · Fuselage Main, Floor BeamSDR UPS07850166Skin · dentedINSPECTION TYPE:C2 DENTS ON NLG RT/STRUT DOOR EXTERIOR SKIN. CUT OUT DAMAGED AREA ON RT/NLG STRUT DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RT/NLG STRUT DOOR IAW SRM 52-02-00 FIG 004.Jul 5, 2007 · N807UP · Doug DC873F · Landing Gear DoorsSDR UPS07850426Fitting · crackedINSPECTION TYPE:C1 FITTING CRACKED AT STA 1160 L19R FWD. REMOVED AND REPLACED LONGERON END FITTING AT STA 1160 L19R IAW SRM 51-1-20D, AND SRM 51-01-24.Jul 4, 2007 · N874UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA07SMN193SPanel · deformedDURING ROUTINE C CHECK INSPECTION; FOUND RIGHT WING INBOARD FLAP LEADING EDGE UPPER PANEL DEFORMED BETWEEN STATION XW 123.000 AND STATION XW 136.000. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. Jul 4, 2007 · N603AL · Doug DC873F · Trailing Edge FlapsSDR UPS07850172Skin · crackedINSPECTION TYPE:C2 CRACK ON EXTERIOR FUSE SKIN AT STA 1740 L19R. CUT OUT DAMAGED AREA ON FUSELAGE SKIN AT STA 1740 L19R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 1740 L19R IAW SRM 53-02-01 FIG 7.Jul 3, 2007 · N807UP · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN187SStringer · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NR 4 MAIN TANK CRACKED STRINGER AT STATION XRS 190.000 AND STRINGER 58. ACCESS THROUGH 505D DOOR. REMOVED FUEL PUMP MOUNT BRACKET. REMOVED DAMAGED AREA AT UPPER HORIZONTAL AND VERTICAL FLANGES. PERFORMED NDT INSPECJun 30, 2007 · N603AL · Doug DC873F · Wing, Longeron/StringerSDR IXXA07SMN184SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MID SHIP ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 660.000 LONGERON 35LEFT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING BETWEEN STATION 660.000 AND LONGERON 35LEFT IAW DC8 SRM 51-1-20D, 51-3-1.Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN179SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LEFT ELEVATOR ON LOWER SKIN AT STATION XE 39.188. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOLJun 30, 2007 · N603AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA07SMN166SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FS 380 LONGERON 33RIGHT, RIGHT FORWARD FUSELAGE JUST AFT OF A-PIT DOOR OPENING. AVERAGE AND MAXIMUM RIVET SPACING EXCEEDED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. RJun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Plate/SkinSDR IXXA07SMN163SSill · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT LONGERON 21 LEFT AT FS 235 MAIN CARGO DOOR LOWER AFT SILL TO AFT JAMB CORNER. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPJun 30, 2007 · N603AL · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA07SMN162SSill · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT MAIN CARGO DOOR COVER SILL AT FS235 LONGERON 21 LT. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, OR CORROSION FOUND. FABRICATED REPAIR PARTS. CLEANED, TREATJun 30, 2007 · N603AL · Doug DC873F · Fuselage Miscellaneous StructureSDR IXXA07SMN174SLongeron · brokenDURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT FLANGE ON LONGERON 19 RIGHT BROKEN AT STATION 200.000 TO 212.000. LONGERON FLANGE FROM AT STATION 200.000 TO 212.000, LONGERON19 RIGHT WAS TRIMMED OFF IN PRODUCTION. NO REPAIR IS REQUIRED. FJun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Longeron/StringerSDR IXXA07SMN191SFloorbeam · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND IN AFT CARGO COMPARTMENT FLOORBEAM UPPER FLANGE SHOWS CORROSION AT STATION 1520.000 RIGHT BOTTOM LINE 44". REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANJun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Floor BeamSDR IXXA07SMN182SBracket · crackedDURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 ALT FUEL TANK BOOSTER PUMP SUPPORTS CRACKED AT STRINGER 59 STATION XW 456.000. REMOVED CRACKED BRACKET. INSTALLED NEW BRACKET AT STATION XW 456.000, STRINGER 59 IAW DC8 SRM 51-1-20D AND 51-3-1.Jun 30, 2007 · N603AL · Doug DC873F · Wing, Attach FittingsSDR IXXA07SMN183SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 1760.000 TO 1766.000 LONGERON 10 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-3-1.Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN185SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND IN MIDSHIP ACCESSORY COMPARTMENT A FITTING CRACKED STATION 660.000 LONGERON 36. REMOVED CRACKED FITTING. INSTALLED NEW FITTING. IAW DC8 SRM 51-1-20D, AND SRM 51-3-1.Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN186SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT LOWER CARGO COMPARTMENT A CRACKED FITTING AT STATION 1180.000 LONGERON 34 RIGHT, AND LONGERON 35 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND SRM 51-3-1.Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN188SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND THE MID ACCESSORY COMPARTMENT FITTING CRACKED BETWEEN STATION 660.000 LONGERON 36 LT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTAJun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN181SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE FITTING CRACKED AT LONGERON 17 RIGHT AT STATION 1768.000. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 51-3-0, 51-3-1, DC8 SRM 51-1-21, 51-3-0, ANJun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN180SFitting · crackedDURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE FITTING HAS A CRACK LONGERON 17 LEFT STATION 1768.000. REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 51-1-20D, 51-3-0, SRM 51-1-8B, DC8 SRM 51-1-21Jun 30, 2007 · N603AL · Doug DC873F · Fuselage Main, Attach FittingsSDR IXXA07SMN178SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LT ELEVATOR LOWER SKIN SHOWS DENT AT STATION XE 55.062. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR AND DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED Jun 30, 2007 · N603AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA07SMN175SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR HAD IMPROPER REPAIR ON LOWER SKIN AT STATION XE 84.968. REMOVED EXISTING. FABRICATED NEW SKIN AND DOUBLER. BONDED BOTH PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSJun 30, 2007 · N603AL · Doug DC873F · Elevator, Plate/SkinSDR IXXA07SMN173SVane · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INTERIM HAD IMPROPER REPAIR AT OUTBOARD VANE SLOT XOLDO 067 AT STATION XFS 566.250. REMOVED EXISTING REPAIR. CUT DAMAGED AREA.PERFORMED NDT INSPECTION. NO CRACK OR CORROSION AFTER CUT. FABRICATED REPAIR PJun 30, 2007 · N603AL · Doug DC873F · Trailing Edge Flaps
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